Finite Element Analysis of Elbow Arthroplasty

DOI : 10.17577/IJERTV6IS040407

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Finite Element Analysis of Elbow Arthroplasty

Vikky Kumhar1*

Department of Mechanical Engineering, Christian College of Engineering and Technology, Bhilai, India

Amit Sarda2

Department of Mechanical Engineering, Christian College of Engineering and Technology, Bhilai, India

Abstract This article provides an information of the biomedical engineering modeling and approach of the elbow arthroplasty process. In this investigation also gives the conceptual design of the total replacement elbow joint which was allows the formulation and analyzing. The complete assembly of elbow model was designed in Creo parametric and analysis done using ANSYS tool, which was gives the results of proposed design and compare between existing and proposed work. Throughout the paper concluded the proposed design was gives the maximum efficient work in suitable material which is cobalt chromium alloys after analysis and comparison in good literature.

Keywords Elbow arthroplasty, finite element analysis, titanium, cobalt chromium, Von-Mises stresses.

*Corrosponding Author

  1. INTRODUCTION

    The elbow implant is used on patients with arm joint pain and disabilities. Samples of conditions inflicting the arthritis and Rheumatoid Arthritis and Osteoarthritis. Arthritis could also be pathologic at intervals that the animal tissue settled in between the humerus and therefore the radius and ulna, that surrounds the joint becomes inflamed and thickened [1]. This may cause harm to the tissue and eventually, pain. Degenerative arthritis joint disease is most generally referred as "wear and tear" arthritis. This disorder happens due to repetitive movement of the joint, inflicting the animal tissue (cartilage) artefact the two bones forming the hinge movement to wear away. because of the animal tissue (cartilage) becomes dilatant, the humerus and radius and ulna would possibly rub against each other, inflicting pain to the elbow.

    Figure 1 elbow implant X-ray images

    1. Link Segment Model

      Link section analysis could also be started with a bottom level approach where ground reaction forces functioning on the feet is entered the model first or a top-down approach where forces

      functioning on the hands area unit accustomed drive the analysis [3]. Link section models are of two types:

      1. Static link section model

      2. Dynamic link section model

    Link section model for the force analysis within the body once a load of specific amount is upraised within the bending condition [3]. The Figure 2 shows the detail link section model drawing of the physique in bend position.

    Figure 2 Human body link segment model

  2. MATERIALS

    For materials to be thought-about a biomaterial it ought to be ready to safely degree dependably replaces or perform in living tissue with an applicable physiological response [5]. In other words, the materials ought to be biocompatible. There are four teams of artificial biomaterials: polymers, metals, ceramics, and composites [5].

    1. Alumina

      The single crystal corundum is hard and powerful but is simply too brittle to be used as articulating part. Like most ceramics, the strength of crystalline corundum is improved by decreasing consistency and grain size [5]. Aluminium oxide implant ought to have a flexural strength and modulus of elasticity of 380GPa to meet ASTM standards F603-78 [5].

    2. Stainless Steel

      The most common form of stainless-steel used for implants is 316L (ASTM F138, F139) [7]. The inclusion of 2.25-3wt.% molybdenum improves salt water corrosion resistance, whereas the drop-in carbon content from 0.08-0.03wt.% maximum improves chloride resolution corrosion resistance.

    3. Cobalt-Chromium Alloys

      The two cobalt-chromium alloys most often need to manufacture implants are CoCrMo (ASTM F75) and CoNiCrMo (ASTM F562). CoCrMo is castable and commonly used in implant applications, whereas CoNiCrMo is hot solid and regularly used to the stem of joint replacements in legs. The properties of CoCrMo ar usually improved by hot isostatic pressing [7]. The addition of chemical element provides the alloy higher strength by preventative grain growth. Despite these variations, however, the trade designation of Vitallium (or within the Great Britain, "Stellite") is often applied erroneously to every alloy. The cobalt-based alloys show a useful balance between mechanical properties and biocompatibility, every type being somewhat superior to stainless-steel in strength and corrosion resistance, however, dearer to manufacture.

    4. Titanium Alloys

    Pure (98.9-99.6%) titanium has four completely different grades, correlating to an increase in impurity content [7]. These impurities, like oxygen, carbon, and nitrogen, greatly influence the mechanical properties of titanium through opening primary solid solution strengthening. Nitrogen offers

    concerning double the strengthening impact per atom, however oxygen content varies the foremost between the grades, rising from 0.18% (grade 1) to 0.40% (grade 4). Hydrogen impurities will harm the malleability of the metallic element through the formation of hydrides [8]. Because of this, the most quantity of hydrogen allowed in titanium element is 0.015wt%. Cold working has been shown to increase the fatigue strength of titanium element [7]. The fatigue strength of pure titanium element is much inferior to alloyed titanium element, it is shown in Table 2.

    TABLE 1 BLOOD COMPATIBILITY PROPERTIES OF BIOMATERIALS.

    S.

    No.

    Properties

    Stiffness

    Strength

    Corrosion resistance

    Blood compatibil

    ity

    1.

    Stainless steel

    Best

    Better

    Good

    Good

    2.

    Co-Cr alloys

    Better

    Good

    Better

    Better

    3.

    Ti-alloys

    Good

    Best

    Best

    Best

    4.

    Polyester

    Good

    High

    High

    Moderate

    5.

    Polytetrafluor

    oethylene

    High

    High

    High

    Low

    6.

    Polyurethanes

    Better

    Medium

    Medium

    Good

    TABLE 2 PROPERTIES OF IMPLANT MATERIALS.

    Materials

    ASTM

    designation

    Condition

    Youngs modulus

    (GPa)

    Yield Strength

    (MPa)

    Tensile Strength

    (MPa)

    Fatigue endurance limit (at 107cycles, R=-1) (MPa)

    Stainless Steel

    F745

    Annealed

    190

    221

    483

    221-280

    F55, F56, F138, F139

    Annealed

    190

    331

    586

    241-276

    30% Cold worked

    190

    792

    930

    310-448

    Cold forged

    190

    1213

    1351

    820

    Co-Cr alloys

    F75

    As-cast/ Annealed

    210

    448-517

    655-889

    207-310

    Powder metallurgy product, hot isostatically pressed

    253

    841

    1277

    725-950

    F562

    Hot forged

    232

    965-1000

    1206

    500

    Cold worked, aged

    232

    1500

    1795

    689-793

    (axial tension R = 0.05, 30 Hz)

    Ti alloys

    F67

    30% Cold-Worked Grade 4

    110

    485

    760

    300

    F136

    Forged Annealed

    116

    896

    965

    620

    Forged, heat treated

    116

    1034

    1103

    620-689

  3. METHODOLOGY

    Elbow, vary of motion of an elbow joint is within the vary from full extension to full flexion. In this section, some mathematical model can be defined for elbow mechanism.

    1. Lever Mechanism in Human Body

      Levers are one amongst the essential tools that were probably employed in prehistoric times. Levers were 1st diagrammatic concerning 260 BC by the standard Greek person Archimedes (287-212 BC). A lever could be a mechanical device that creates work easier for use; it involves moving a load around a pivot employing a force. Several of our basic tools use levers, together with scissors, pliers, hammer claws, nutcrackers, and tongs.

      Their lever mechanism is classified into three class they are following [18]:

      • The lever Class One, the pivot (fulcrum) is between the effort (force) and the weight.

      • The Lever Class Second, the weight is between the pivot and the effort (force) and

      • The Lever Class Three, the effort is between the pivot and the weight or load.

        Figure 3 Free body diagram of elbow

    2. Equations of Arm Mechanism

      From the free body diagram in Figure 5, several equations were derived to calculate all four forces to be put in finite element analysis. The derived equations were;

      Moments about Elbow joint = 0,

      ——————(1)

      are perpendicular measured distances from the elbow joint.

      After the force acted by the biceps was calculated, the sum of the moment in the 'y-axis' direction will be taken as zero.

      Sum of moments on 'y-axis' = 0,

      ——————-(2)

      G is the weight of the forearm with an account of the gravitational force, acting vertically downwards. B is the force acted by the biceps, W is the weight of the object and R is the reaction force of the joint.

    3. Modelling and Analysis

      The models have created in Creo Parametric software tool. Figure 4 has been shows that the existing modeling, proposed model has been modeled by changing existing design and surface geometry of model from sharp edge to smooth edges as shown in Figure 5.

      Figure 4 Total replacement joint existing model

      Figure 5 Total replacement joint proposed model

      Figure 6 Meshing view of proposed model

    4. Boundary Conditions

    All four forces were calculated and compiled for boundary conditions as shown in TABLE 3, shows the forces applied for all three materials [21].

    TABLE 3 FORCES APPLIED TO THE ALL MATERIALS ELBOW MODAL [21].

    Conditions

    Force, N

    G

    W

    B

    R

    0.1kg,

    6.867

    0.981

    50.458

    34.762

    0.1kg,

    6.867

    0.981

    25.229

    17.381

    0.1kg,

    6.867

    0.981

    32.934

    22689

    0.5kg,

    6.867

    4.905

    95.309

    71765

    0.5kg,

    6.867

    4.905

    47.654

    35.882

    0.5kg,

    6.867

    4.905

    62.209

    46.481

    1.5kg,

    6.867

    14.715

    207.437

    164273

    1.5kg,

    6.867

    14.715

    103.719

    82137

    1.5kg,

    6.867

    14.715

    135.395

    107.222

    2.5kg,

    6.867

    24.525

    319.566

    256.391

    2.5kg,

    6.867

    24.525

    159.783

    128.391

    2.5g,

    6.867

    24.525

    208.582

    167.602

  4. RESULTS AND DISCUSSIONS

    For this investigation, the criterions were viewed from the ANSYS 16.2, that are gives the Equivalent (von-Mises) Stress and a Principal Stress as shown in Figure 7 & 8. The various results from ANSYS 16.2 exploitation whole completely different cases.

    (a) (b)

    (c) (d)

    Figure 7 Von-Mises Stress in proposed elbow joint for different materials (a)

    Copper (B) Stainless Steel (c) Titanium and (d) Cobalt chromium alloy

    (a) (b)

    (c) (d)

    Figure 8 Von-Mises Stress in proposed elbow joint for different materials (a) Copper (B) Stainless Steel (c) Titanium and (d) Cobalt chromium alloy

    TABLE 4 RESULT OF VON-MISES STRESS FOR EXISTING MODEL

    The Table 4 indicates that the validation results between existing and Khoo et. al., work.

    Figure 9 Comparison of von mises stress between existing model and proposed model for all materials

    Figure 10 Comparison max principal stress between existing model and proposed model for all materials

    Figure 9 and 10, shows a comparison between existing model and proposed model for the different materials, such as copper, stainless steel, titanium and cobalt chromium. Proposed model gives 12.477% less von mises stress and 14.030% less maximum principal stress generation as compare to existing model respectively.

    TABLE 5 COMPARISON BETWEEN EXISTING WORK WITH PROPOSED WORK

    Stress

    Titanium (Khoo et. al. (Existing

    work)

    Cobalt-Chromium with Proposed Model (Proposed work)

    %

    Difference

    Von-Mises

    42.365

    37.079

    12.477

    Max

    Principal

    39.299

    33.785

    14.030

    S. No.

    Material

    Khoo et. al. (Exist

    Model)

    Validation

    % Error

    1

    Copper

    45.755

    45.1

    1.4315

    2

    Stainless Steel

    45.04

    44.838

    0.4485

    3

    Titanium

    42.365

    42.085

    0.6609

  5. CONCLUSION

In this article, the applications of the biomaterial cobalt chromium metal for elbow arthroplasty implant has been proposed for higher performance. The proposed model performs the less von-mises stress generation as compare to existing implant. The comparisons of the each existing [7] and proposed model (present work) simulated results for identical environmental setups. Table 1, shown that relative differences between the commonly used metallic alloys or polymers as biomaterials, which clarify that the cobalt chromium has a better blood compatibility for the human body. The von mises and maximum principal stress percentage error between the existing work and the proposed work are 12.477% and 14.030% respectively is shown in Table 5, which is under design safe. Due to modification of design and surface conditions, the weight of proposed model was less as compare to existing and cost are also reduced, therefore the cobalt chromium is suitable for proposed design and existing design. By using cobalt chromium which will also result in a minimal principal stress on the implant.

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